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COSMOS 2466 (GLONASS), 37137

Orbit data source: Space-Track

COSMOS 2466 (GLONASS), 37137 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Thu, 02 Sep 2010 UTC via a PROTON-M/DM-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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COSMOS 2466 (GLONASS) details

Identifier	37137, 2010-041A
Orbit	MEO
Last TLE update	9 hours ago
Origin	KVR/IACG (CIS)
Manufacturer	Resehetnev ISS
Mission	Non-operational Defense Navigation
Bus & Motor	URAGAN, Unknown motor
Mass	1,450 kg wet, ~1,200 kg dry
Launch date (UTC)	2010-09-02 (14 years ago)
Launch vehicle	PROTON-M/DM-2
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + 1 Ant + 2 Pan, 7.8 m
Radar Cross Section	8.467 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 COSMOS 2466 (GLONASS)
1 37137U 10041A   24361.07545149  .00000113  00000-0  00000+0 0  9992
2 37137  63.8927 208.5293 0016943 167.2568   4.9072  2.13113183111430

Epoch: 2024-12-26T01:48Z

Definitive object data (Epoch: 2024-12-26T01:48:39.008Z)

Latitude	7.04441°
Longitude	-97.15661°
Altitude	19,085.863 km
Speed	3.96 km/s
True Right ascension	01h 40m 15s
True Declination	7° 01' 58"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	54.6377°
Longitude	-137.32185°
Altitude	19,110.753 km
Speed	3.958 km/s
Apparent Right ascension	22h 54m 18s
Apparent Declination	40° 21' 28"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	10:38:21
Azimuth	356.918° N
Elevation	-9.644°
Doppler factor	1

Orbital elements

Apogee altitude	19,171.865 km
Perigee altitude	19,085.433 km
Semi-major axis	25,506.786 km
Eccentricity	0.0016943
Inclination	63.8927°
RAAN	208.5293°
Arg. of periapsis	167.2568°
True anomaly	4.92384°
Mean anomaly	4.9072°
Eccentric anomaly	4.91552°
Mean motion	0.53279 °/min
BSTAR	Unknown
Orbital period	675.68 mins